CA2884233C - Procede et systeme de demarrage d'un turbomoteur d'aeronef - Google Patents

Procede et systeme de demarrage d'un turbomoteur d'aeronef Download PDF

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Publication number
CA2884233C
CA2884233C CA2884233A CA2884233A CA2884233C CA 2884233 C CA2884233 C CA 2884233C CA 2884233 A CA2884233 A CA 2884233A CA 2884233 A CA2884233 A CA 2884233A CA 2884233 C CA2884233 C CA 2884233C
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Prior art keywords
shaft
acceleration
during
starter
starting
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CA2884233A
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English (en)
French (fr)
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CA2884233A1 (fr
Inventor
Pierre Harriet
Jean Philippe Jacques Marin
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Turbomeca SA
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Publication of CA2884233A1 publication Critical patent/CA2884233A1/fr
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D19/00—Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275—Mechanical drives
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/85—Starting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/04—Purpose of the control system to control acceleration (u)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/304—Spool rotational speed
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/309—Rate of change of parameters

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
CA2884233A 2012-09-10 2013-08-27 Procede et systeme de demarrage d'un turbomoteur d'aeronef Active CA2884233C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1258460 2012-09-10
FR1258460A FR2995345B1 (fr) 2012-09-10 2012-09-10 Procede et systeme de demarrage d'un turbomoteur d'aeronef
PCT/FR2013/051977 WO2014037649A1 (fr) 2012-09-10 2013-08-27 Procédé et système de démarrage d'un turbomoteur d'aeronef

Publications (2)

Publication Number Publication Date
CA2884233A1 CA2884233A1 (fr) 2014-03-13
CA2884233C true CA2884233C (fr) 2020-05-12

Family

ID=47739376

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2884233A Active CA2884233C (fr) 2012-09-10 2013-08-27 Procede et systeme de demarrage d'un turbomoteur d'aeronef

Country Status (12)

Country Link
US (1) US9874149B2 (enExample)
EP (1) EP2893169B1 (enExample)
JP (1) JP2015529770A (enExample)
KR (1) KR20150054854A (enExample)
CN (1) CN104884769B (enExample)
CA (1) CA2884233C (enExample)
ES (1) ES2624640T3 (enExample)
FR (1) FR2995345B1 (enExample)
IN (1) IN2015DN01835A (enExample)
PL (1) PL2893169T3 (enExample)
RU (1) RU2646521C2 (enExample)
WO (1) WO2014037649A1 (enExample)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3022601B1 (fr) * 2014-06-19 2016-06-10 Valeo Embrayages Estimateur de couple pour double embrayage
FR3025252B1 (fr) * 2014-08-29 2021-10-29 Microturbo Dispositif et procede de demarrage d'une turbine a gaz, procede de regulation de la vitesse de rotation d'une turbine a gaz, et turbine a gaz et turbomoteur associes
US10502139B2 (en) 2015-01-28 2019-12-10 General Electric Company Method of starting a gas turbine engine including a cooling phase
AU2015401568A1 (en) * 2015-07-08 2018-01-18 Ge Aviation Systems Llc Air starter and methods for determining hydrostatic lock
CN105545492A (zh) * 2015-12-10 2016-05-04 陕西航空电气有限责任公司 一种航空发动机的多段式加速度起动控制方法
FR3063782B1 (fr) * 2017-03-07 2021-06-18 Safran Aircraft Engines Procede et dispositif de detection de conditions propices a l'apparition d'un pompage en vue de proteger un compresseur d'une turbomachine d'aeronef
US10352189B2 (en) * 2017-05-10 2019-07-16 Pratt & Whitney Canada Corp. Method and system for setting an acceleration schedule for engine start
US10006375B1 (en) * 2017-07-11 2018-06-26 General Electric Company Propulsion system for an aircraft
FR3074836B1 (fr) * 2017-12-13 2019-11-15 Safran Aircraft Engines Procede de detection d'allumage de turbomachine
FR3076322B1 (fr) * 2017-12-29 2021-09-24 Safran Aircraft Engines Procede et dispositif de demarrage pour une turbomachine par temps froid
CN108757186B (zh) * 2018-05-11 2019-08-27 中国航发动力股份有限公司 一种燃气轮机数字式转速控制系统及方法
CN110886656B (zh) * 2018-09-11 2024-06-18 普拉特-惠特尼加拿大公司 用于为发动机启动设定加速度计划的方法与系统
US11073086B2 (en) * 2018-11-27 2021-07-27 The Boeing Company Apparatus, assemblies, and methods for mitigating thermal bow in the rotor of an engine at start-up
GB201819695D0 (en) * 2018-12-03 2019-01-16 Rolls Royce Plc Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine
GB201819696D0 (en) * 2018-12-03 2019-01-16 Rolls Royce Plc Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine
FR3101918B1 (fr) * 2019-10-15 2023-03-31 Safran Aircraft Engines Procédé de démarrage d’un turbomoteur, Dispositif, turbomoteur, AERONEF et produit programme d’ordinateur
US20210172376A1 (en) * 2019-12-10 2021-06-10 General Electric Company Combustor ignition timing
CN113266474B (zh) * 2021-06-01 2022-07-15 中国航空工业集团公司沈阳飞机设计研究所 一种加载条件下的航空发动机起动阻力矩测量方法
FR3124225B1 (fr) 2021-06-18 2023-06-02 Safran Système de propulsion d’un aéronef avec dispositif de commande de démarrage
CN114034489B (zh) * 2022-01-10 2022-03-25 成都中科翼能科技有限公司 一种燃气涡轮发动机地面起动加速时间计算方法
CN115075954B (zh) * 2022-05-23 2023-03-28 蓝箭航天空间科技股份有限公司 提高发动机启动成功率的方法及装置
US12428997B2 (en) 2024-01-23 2025-09-30 Rtx Corporation Multi-mode starter control for gas turbine engines

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58187529A (ja) * 1982-04-28 1983-11-01 Hitachi Ltd ガスタ−ビン装置
EP0623741B1 (en) * 1993-03-16 2001-06-06 AlliedSignal Inc. Gas turbine starter assist torque control system
US5430362A (en) * 1993-05-12 1995-07-04 Sundstrand Corporation Engine starting system utilizing multiple controlled acceleration rates
RU2050455C1 (ru) * 1993-11-22 1995-12-20 Анатолий Михайлович Рахмаилов Способ запуска газотурбинного двигателя и газотурбинный двигатель
US5844383A (en) * 1997-07-15 1998-12-01 Sundstrand Corporation Gas turbine engine starting system and method
JP2003201864A (ja) * 2002-01-09 2003-07-18 Ebara Corp ガスタービン装置の起動方法及びガスタービン装置
US7840333B2 (en) * 2007-03-30 2010-11-23 Hamilton Sundstrand Corporation Event-driven starter controller
FR2915238A1 (fr) * 2007-04-23 2008-10-24 Airbus France Sa Procede et systeme pour le demarrage d'un turbomoteur par temps froid.
US8245517B2 (en) * 2009-05-19 2012-08-21 Hamilton Sundstrand Corporation Gas turbine starting with stepping speed control
US8925328B2 (en) 2009-10-26 2015-01-06 Siemens Energy, Inc. Gas turbine starting process
US8479522B2 (en) * 2009-12-23 2013-07-09 General Electric Company Method of starting a turbomachine by testing operational support systems during the purging process
US8833085B2 (en) * 2010-01-27 2014-09-16 General Electric Company System and method for gas turbine startup control
US9145833B2 (en) * 2010-05-25 2015-09-29 General Electric Company Gas turbine startup control
US8955334B2 (en) * 2010-07-22 2015-02-17 General Electric Company Systems and methods for controlling the startup of a gas turbine

Also Published As

Publication number Publication date
US20150211421A1 (en) 2015-07-30
RU2646521C2 (ru) 2018-03-05
IN2015DN01835A (enExample) 2015-05-29
PL2893169T3 (pl) 2017-08-31
KR20150054854A (ko) 2015-05-20
FR2995345A1 (fr) 2014-03-14
US9874149B2 (en) 2018-01-23
CN104884769A (zh) 2015-09-02
JP2015529770A (ja) 2015-10-08
FR2995345B1 (fr) 2018-06-15
WO2014037649A1 (fr) 2014-03-13
CN104884769B (zh) 2017-05-17
EP2893169B1 (fr) 2017-04-05
CA2884233A1 (fr) 2014-03-13
RU2015107555A (ru) 2016-10-27
ES2624640T3 (es) 2017-07-17
EP2893169A1 (fr) 2015-07-15

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